I'd need some help with the following question:
Aircraft is flying at FL 350 with Mach 0.878 OAT = ISA + 4°C. Compressibility Factor is 0.939. Calculate TAS.
Correct answer would be 510 kts.
Her are my steps, but my result doesn't even come close to the answer given.
- determine OAT at FL 350 = - 51°C
- calculate LSS = 0.878 (Mach) x 38.9 (square route out of) 222 = 508 kts
- 508 kts x 0.939 (C. Factor) = 478 TAS